Keyphrases
Beam Model
18%
Composite Timoshenko Beam
30%
Computer Package
26%
Differential Equations of Motion
69%
Differential Transform Method
79%
Double-tapered
40%
Equations of Motion
63%
Euler-Bernoulli Beam
25%
Finite Element Formulation
16%
Finite Element Method
20%
Flapwise Bending Vibration
73%
Flight Condition
13%
Flutter Analysis
20%
Flutter Stability
10%
Flutter Vibration
10%
Free Vibration Analysis
78%
Functionally Graded
13%
Functionally Graded Beam
16%
Governing Differential Equation
49%
Hamilton's Principle
32%
Helicopter Blade
26%
Hingeless Rotor
13%
Hovering
20%
Hovering Flight
13%
Hub Radius
57%
Index Parameters
13%
Kinetic Energy
18%
Material Properties
26%
Mathematica
26%
Mathematical Techniques
32%
Mode Shape
16%
Natural Frequency
72%
Ply Orientation
21%
Potential Energy
27%
Power-law Index
13%
Rotary Inertia
32%
Rotating Timoshenko Beam
23%
Rotational Speed
45%
Rotor Blade
16%
Shear Deformation
37%
Slenderness Ratio
43%
Stability Analysis
20%
Taper Ratio
26%
Tapered Beam
13%
Tapered Timoshenko Beam
20%
Timoshenko Beam
32%
Torsional Vibration
13%
Twist-stretch Coupling
23%
Vibration Analysis
100%
Vibration Characteristics
11%
Engineering
Aerodynamic Load
10%
Angular Velocity ω
6%
Aspect Ratio
55%
Axial Direction
5%
Axial Force
5%
Beam Model
25%
Bending Vibration
85%
Bernoulli Beam
15%
Blade Element
10%
Blade Model
5%
Blade Turbine
5%
Boundary Condition
45%
Characteristic Vibration
8%
Composite Section
10%
Deformation Ratio
10%
Dynamic Property
15%
Engineering Application
15%
Euler Beam
10%
Finite Element Analysis
36%
Finite Element Formulation
18%
Finite Element Modeling
10%
Flight Condition
13%
Free Vibration
30%
Free Vibration Analysis
85%
Functionally Graded Material
10%
Good Agreement
36%
Governing Differential Equation
58%
Hamilton's Principle
43%
Helicopter Blade
30%
Kinetic Study
10%
Mathematical Technique
45%
Mode Shape
20%
Numerical Example
15%
Perturbation Equation
6%
Ply Orientation
23%
Potential Energy
30%
Power Law Index
20%
Resonant Frequency
93%
Rotary Inertia
45%
Rotational Speed
63%
Rotor Blade
16%
Shear Deformation
50%
Stability Analysis
10%
Structural Property
5%
System Efficiency
5%
Thickness Direction
5%
Thin-Walled Composite Beam
10%
Torsional Vibration
15%
Turbine Components
10%
Vibration Analysis
100%